US2575973A - Tangential acceleration gauge - Google Patents
Tangential acceleration gauge Download PDFInfo
- Publication number
- US2575973A US2575973A US483301A US48330143A US2575973A US 2575973 A US2575973 A US 2575973A US 483301 A US483301 A US 483301A US 48330143 A US48330143 A US 48330143A US 2575973 A US2575973 A US 2575973A
- Authority
- US
- United States
- Prior art keywords
- housing
- projectile
- gage
- balls
- recess
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000001133 acceleration Effects 0.000 title description 13
- 239000002184 metal Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 238000010276 construction Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/04—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses for indicating maximum value
- G01P15/06—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses for indicating maximum value using members subjected to a permanent deformation
Definitions
- TANGENTIAL ACCELERATION GAUGE Filed April 16, 1943 FI6.6. ⁇ w 270 b o/mcr a o ROTATION 28 was due. housing is provided with two sets of relatively Patented Nov. 20, 1951 UNITED STATES PATENT OFFICE 2,575,973 TANGENTIAL ACCELERATION GAUGE Thomas M. Perry, Bennington, Vt., assignor to the United States of America as represented by the Secretary of the Navy Application April 16, 1943, Serial N 0. 483,301
- This invention relates to measuring devices and has particular reference to a novel gage for measuring the angular or. tangential acceleration of rotary projectiles.
- Another object of the invention is to provide a tangential acceleration gage of simple construction which is designed for manufacture at low cost and provides accurate measurements.
- FIG. 1 is an elevation of a gage embodying one form of the invention, a portion of the projectile being shown in phantom lines, to show the location of the gage;
- Fig. 2 is a perspective view of a cover for the gage shown in Fig. 1;
- Fig. 3 is a perspective view of the main body of the gage
- Fig. 4 is a transverse sectional view on line 4-4 of Fig. 1' of the gage showing the parts in their normal positions prior to firing of the projectile;
- Fig. 5 is an enlarged transverse sectional view of part of the gage showing the final positions of the parts after the projectile is fired
- Fig. 6 is a view similar to Fig. 4 showing a modified form of the gage.
- the gage I0 embodying the invention is shown mounted in a projectile comprising a hollow casing H and a nose portion I2 threaded in'the front end of the casing.
- the gage is mounted in the casing H by any suitable means (not shown) for securing the gage against movement relative to the casing.
- the gage comprises a cylindrical housing 14, which may be made of metal, having a pair of diametrically opposed recesses 15 andl5a. in its front end.
- the recesses as shown, are cylinders, whose axes extend parallel to the axis of rotation of the housing and which terminate short
- the bases of the cylinders are generally elliptical with their 'major axes extending at right angles to the common diameter on which the recesses lie.
- a relatively small bore screw I1 threaded in the housing.
- a similar bore Ifia communicates with the end of therecess [5a remote from the bore IS, the outer end of the bore liia being closed by a plug or screw Ha.
- the recesses l5 and l5a contain relatively hard balls 18 and 18a, respectively, which may be made of steel, the balls being movable freely in the recesses along their major axes.
- Within the bores l6 and l6a. are relatively soft balls l9 and ma, respectively, which may be made of copper, or the like.
- the balls l9 and Mia, as shown, are confined in the bores by the plugs l1 and Ha, respectively, so that part of each ball projects into the adjacent recess.
- a cover plate 20 is preferably secured on the front face of the housing to retain the balls 48 and l8a in their re spective recesses, and to prevent axial shift of said balls, as will be clear from Fig. 1.
- the relatively soft balls 19 and HM are compressed and distorted by pushing against the harder balls i8 and Ida, as shown in Fig. 5, because of the inertial resistance or" the harder balls against the parts of the balls l9 and Na projecting into the recesses.
- the. gage is removed from the casing II, and the balls l9 and l9a, are removed from the housing Id by unscrewing the plugs l1 and l'la. l9 and l9a may then be determined, which gives a measure of the maximum angular or tangential acceleration of the projectile during its flight.
- the gage shown in Fig. 6 comprises a cylindrical housing 23 having an offset recess 24 in its front end. As shown, the recess 24 is made up of two generally rectangular, diametrically opposed chambers having adjacent corners co inciding at the axis of rotation of the housing.
- -A lever 25 is pivotally mounted in the recess on of the recess but being somewhat smaller so that it may swing in the recess on the pivot pin.
- Near the ends of the recess are bores2l and 21a which extend outwardly in opposite directions and are closed at their outer ends by plugs 28 and 28a, respectively, threaded in the housing.
- the bores 21 and 21a communicate with the recess and contain relatively soft metal'balls 29 and 29a, respectively, confined between the plugs and the adjacent ends of the lever, which is made of a relatively hard metal, such as steel.
- the new gage may be made in a compact form and is of a rugged construction having only a deformation of the others
- the amount of distortion of the balls What is claimed is:
- a tangential acceleration gage for a spinningtest projectile comprising a cylindrical housing designed to be mounted within said projectile with the axis of the housing alined with the spin aXis of the projectile, said housing having two similar recesses located symmetrically with respect to the said axis, two equal large and relatively massive hardened steel spheres, one in each recess, each said recess being substantially a right circular cylinder whose diameter and length are the'same as the diameter of the sphere therein, but each said recess being slightly elongated in a direction chordal to the housing, thus permitting'a slight amount of play of said sphere,
- each recess having in its side wall a smooth bore of a diameter relatively small with respect to the diameter of the spheres, the axes of said bores passing through the centers of the spheres andbeing in the plane transverse to the axis of the housing including said centers, said bores extending in opposite directions with respect to the straight line connecting said centers, a'small sphere of soft metal fitting in each bore, ea'ch bore having a screw threaded extension at its end remote fromthe corresponding recess, a
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Description
Nov. 20, 1951 'r. M. PERRY 2,575,973
TANGENTIAL ACCELERATION GAUGE Filed April 16, 1943 FI6.6. \w 270 b o/mcr a o ROTATION 28 was due. housing is provided with two sets of relatively Patented Nov. 20, 1951 UNITED STATES PATENT OFFICE 2,575,973 TANGENTIAL ACCELERATION GAUGE Thomas M. Perry, Bennington, Vt., assignor to the United States of America as represented by the Secretary of the Navy Application April 16, 1943, Serial N 0. 483,301
This invention relates to measuring devices and has particular reference to a novel gage for measuring the angular or. tangential acceleration of rotary projectiles.
relatively hard element, preferably of metal, is
disposed in the recess adjacent a relatively soft element, and one of the elements is secured against movement with respect to the housing by suitable means in said housing. The other element is not secured to the housing and fits loosely in the recess, so that while angular acceleration is being imparted to the housing by the spin of the projectile produced by the rifling of the gun on firing, the said unsecured element will tend to remainat rest, due to its own inertia, and thus the secured element will press against it. As a result both elements will become distorted at the region of contact, the softer one,
of course, to a greater extent than the other.
-Measurement of such distortion provides an indication oi the angular acceleration to which it In the preferred, construction, the
movable elements disposed in diametrically opposed relation so that the gage does not affect the balance of the projectile with respect to its axis of rotation.
Another object of the invention is to provide a tangential acceleration gage of simple construction which is designed for manufacture at low cost and provides accurate measurements.
These and other objects of the invention may be understood by reference to the accompanying drawing, wherein Fig. 1 is an elevation of a gage embodying one form of the invention, a portion of the projectile being shown in phantom lines, to show the location of the gage;
Fig. 2 is a perspective view of a cover for the gage shown in Fig. 1;
Fig. 3 is a perspective view of the main body of the gage;
Fig. 4 is a transverse sectional view on line 4-4 of Fig. 1' of the gage showing the parts in their normal positions prior to firing of the projectile;
1 Claim. (01. 264-1) of the rear end thereof.
Fig. 5 is an enlarged transverse sectional view of part of the gage showing the final positions of the parts after the projectile is fired, and
Fig. 6 is a view similar to Fig. 4 showing a modified form of the gage.
Referring first to Figs. 1 to 6 of the drawin the gage I0 embodying the invention is shown mounted in a projectile comprising a hollow casing H and a nose portion I2 threaded in'the front end of the casing. The gage is mounted in the casing H by any suitable means (not shown) for securing the gage against movement relative to the casing.
The gage comprises a cylindrical housing 14, which may be made of metal, having a pair of diametrically opposed recesses 15 andl5a. in its front end. The recesses, as shown, are cylinders, whose axes extend parallel to the axis of rotation of the housing and which terminate short Preferably, the bases of the cylinders are generally elliptical with their 'major axes extending at right angles to the common diameter on which the recesses lie. At one end of the recess I5 is a relatively small bore screw I1 threaded in the housing. A similar bore Ifia communicates with the end of therecess [5a remote from the bore IS, the outer end of the bore liia being closed by a plug or screw Ha.
The recesses l5 and l5a contain relatively hard balls 18 and 18a, respectively, which may be made of steel, the balls being movable freely in the recesses along their major axes. Within the bores l6 and l6a. are relatively soft balls l9 and ma, respectively, which may be made of copper, or the like. The balls l9 and Mia, as shown, are confined in the bores by the plugs l1 and Ha, respectively, so that part of each ball projects into the adjacent recess. A cover plate 20 is preferably secured on the front face of the housing to retain the balls 48 and l8a in their re spective recesses, and to prevent axial shift of said balls, as will be clear from Fig. 1.
In operation, when the projectile is fired from a gun, the usual rifling in the gun barrel causes the projectile to rotate at a speed which accelerates rapidly as the projectile moves through the barrel, the rotation of the projectile here being assumed in such a direction that the housing [4 moves counterclockwise as shown in Fig. 4. Accordingly, the balls l8 and 18a move relatively outwardly in their recesses against the balls is and [9a, respectively, due to centrifugal force and the inertia of the balls I8, I80. incident to the angular acceleration of the projectile. As
a result, the relatively soft balls 19 and HM are compressed and distorted by pushing against the harder balls i8 and Ida, as shown in Fig. 5, because of the inertial resistance or" the harder balls against the parts of the balls l9 and Na projecting into the recesses. When the projectile is recovered, the. gage is removed from the casing II, and the balls l9 and l9a, are removed from the housing Id by unscrewing the plugs l1 and l'la. l9 and l9a may then be determined, which gives a measure of the maximum angular or tangential acceleration of the projectile during its flight. The gage shown in Fig. 6 comprises a cylindrical housing 23 having an offset recess 24 in its front end. As shown, the recess 24 is made up of two generally rectangular, diametrically opposed chambers having adjacent corners co inciding at the axis of rotation of the housing.
-A lever 25 is pivotally mounted in the recess on of the recess but being somewhat smaller so that it may swing in the recess on the pivot pin. Near the ends of the recess are bores2l and 21a which extend outwardly in opposite directions and are closed at their outer ends by plugs 28 and 28a, respectively, threaded in the housing. The bores 21 and 21a, communicate with the recess and contain relatively soft metal'balls 29 and 29a, respectively, confined between the plugs and the adjacent ends of the lever, which is made of a relatively hard metal, such as steel. When the projectile is being fired from a gun, the housing 23 rotates counterclockwise (Fig. 6) with a high angular acceleration, and the lever 25, due to its inertia, resists being set into corresponding rotation about the pin 26. The relatively soft balls 29 and 29a, therefore, are compressed and distorted by the forces they exert against the adjacent ends of the lever, in imparting the necessary acceleration to said lever, to make it rotate with the housing, the amount of the distortion depending upon the rate of angular acceleration of the projectile. By unscrewing the plugs 28 and 28a, the balls may be removed from the housing 23 to permit measurement of their deformation. 7
The new gage may be made in a compact form and is of a rugged construction having only a deformation of the others The amount of distortion of the balls What is claimed is:
A tangential acceleration gage for a spinningtest projectile, comprising a cylindrical housing designed to be mounted within said projectile with the axis of the housing alined with the spin aXis of the projectile, said housing having two similar recesses located symmetrically with respect to the said axis, two equal large and relatively massive hardened steel spheres, one in each recess, each said recess being substantially a right circular cylinder whose diameter and length are the'same as the diameter of the sphere therein, but each said recess being slightly elongated in a direction chordal to the housing, thus permitting'a slight amount of play of said sphere,
each recess having in its side wall a smooth bore of a diameter relatively small with respect to the diameter of the spheres, the axes of said bores passing through the centers of the spheres andbeing in the plane transverse to the axis of the housing including said centers, said bores extending in opposite directions with respect to the straight line connecting said centers, a'small sphere of soft metal fitting in each bore, ea'ch bore having a screw threaded extension at its end remote fromthe corresponding recess, a
screw therein, and a shoulder at the junction of r the smooth bore and the screw threaded-extension thereof to form 'an abutment for the inner end of said screw, whereby each small sphere is caused to extend a predetermined distance into the adjacent recess when the inner end of the screw engages said small sphere and the corresponding abutment. I
' THOMAS M. PERRY.
' REFERENCES CITED The. following references are of record in the file of this patent: 1
UNITED STATES PATENTS
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US483301A US2575973A (en) | 1943-04-16 | 1943-04-16 | Tangential acceleration gauge |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US483301A US2575973A (en) | 1943-04-16 | 1943-04-16 | Tangential acceleration gauge |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2575973A true US2575973A (en) | 1951-11-20 |
Family
ID=23919526
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US483301A Expired - Lifetime US2575973A (en) | 1943-04-16 | 1943-04-16 | Tangential acceleration gauge |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2575973A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2721071A (en) * | 1952-04-14 | 1955-10-18 | Marvin L Kempton | Apparatus for measuring transverse accelerations |
| US2970010A (en) * | 1957-09-30 | 1961-01-31 | Lyon George Albert | Wheel cover |
| US2986930A (en) * | 1957-11-07 | 1961-06-06 | Ryan Aeronautical Co | Engine trunnion mounting and thrust indicating means |
| US3103120A (en) * | 1961-10-04 | 1963-09-10 | Joseph F Tinney | Omnidirectional "g" switch |
| US3141440A (en) * | 1962-04-02 | 1964-07-21 | Fletcher N Platt | Impact recording instrument |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH7161A (en) * | 1893-08-04 | 1894-01-31 | Metallpatronenfabrik Deutsche | Gas pressure gauges for rifles and cannons with central ignition |
| US993091A (en) * | 1908-01-14 | 1911-05-23 | Bethlehem Steel Corp | Time-fuse for projectiles. |
| US1310892A (en) * | 1919-07-22 | Eugene schneider | ||
| US1870405A (en) * | 1931-08-14 | 1932-08-09 | Thomas B Doe | Fuse for antiaircraft projectiles |
| US2155635A (en) * | 1938-05-02 | 1939-04-25 | Continental Oil Co | Bottom hole pressure gauge |
| US2195451A (en) * | 1937-09-16 | 1940-04-02 | Illinois Testing Laboratories | Weighing apparatus |
| US2263512A (en) * | 1939-01-23 | 1941-11-18 | James T Logan | Electrical supervision |
| US2362123A (en) * | 1940-08-08 | 1944-11-07 | Ford Instr Co Inc | Fuse |
| US2390581A (en) * | 1943-02-22 | 1945-12-11 | Honeywell Regulator Co | Control device |
| US2436529A (en) * | 1944-05-05 | 1948-02-24 | Farnsworth Res Corp | Inertia tripping mechanism |
| US2445307A (en) * | 1943-03-31 | 1948-07-13 | Us Navy | Force gauge |
-
1943
- 1943-04-16 US US483301A patent/US2575973A/en not_active Expired - Lifetime
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1310892A (en) * | 1919-07-22 | Eugene schneider | ||
| CH7161A (en) * | 1893-08-04 | 1894-01-31 | Metallpatronenfabrik Deutsche | Gas pressure gauges for rifles and cannons with central ignition |
| US993091A (en) * | 1908-01-14 | 1911-05-23 | Bethlehem Steel Corp | Time-fuse for projectiles. |
| US1870405A (en) * | 1931-08-14 | 1932-08-09 | Thomas B Doe | Fuse for antiaircraft projectiles |
| US2195451A (en) * | 1937-09-16 | 1940-04-02 | Illinois Testing Laboratories | Weighing apparatus |
| US2155635A (en) * | 1938-05-02 | 1939-04-25 | Continental Oil Co | Bottom hole pressure gauge |
| US2263512A (en) * | 1939-01-23 | 1941-11-18 | James T Logan | Electrical supervision |
| US2362123A (en) * | 1940-08-08 | 1944-11-07 | Ford Instr Co Inc | Fuse |
| US2390581A (en) * | 1943-02-22 | 1945-12-11 | Honeywell Regulator Co | Control device |
| US2445307A (en) * | 1943-03-31 | 1948-07-13 | Us Navy | Force gauge |
| US2436529A (en) * | 1944-05-05 | 1948-02-24 | Farnsworth Res Corp | Inertia tripping mechanism |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2721071A (en) * | 1952-04-14 | 1955-10-18 | Marvin L Kempton | Apparatus for measuring transverse accelerations |
| US2970010A (en) * | 1957-09-30 | 1961-01-31 | Lyon George Albert | Wheel cover |
| US2986930A (en) * | 1957-11-07 | 1961-06-06 | Ryan Aeronautical Co | Engine trunnion mounting and thrust indicating means |
| US3103120A (en) * | 1961-10-04 | 1963-09-10 | Joseph F Tinney | Omnidirectional "g" switch |
| US3141440A (en) * | 1962-04-02 | 1964-07-21 | Fletcher N Platt | Impact recording instrument |
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